US4572123A - Internal combustion engine squish jet combustion chamber - Google Patents

Internal combustion engine squish jet combustion chamber Download PDF

Info

Publication number
US4572123A
US4572123A US06/623,740 US62374084A US4572123A US 4572123 A US4572123 A US 4572123A US 62374084 A US62374084 A US 62374084A US 4572123 A US4572123 A US 4572123A
Authority
US
United States
Prior art keywords
bowl
outlets
squish
jet passages
pair
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US06/623,740
Inventor
Robert L. Evans
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
University of British Columbia
Original Assignee
University of British Columbia
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by University of British Columbia filed Critical University of British Columbia
Priority to US06/623,740 priority Critical patent/US4572123A/en
Assigned to UNIVERSITY OF BRITISH COLUMBIA THE reassignment UNIVERSITY OF BRITISH COLUMBIA THE ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: EVANS, ROBERT L.
Application granted granted Critical
Publication of US4572123A publication Critical patent/US4572123A/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00Engines characterised by precombustion chambers
    • F02B19/14Engines characterised by precombustion chambers with compression ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0627Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion having additional bores or grooves machined into the piston for guiding air or charge flow to the piston bowl
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/063Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion the combustion space in the piston interacting fluid dynamically with the cylinder head, the injector body or the cylinder wall
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0636Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom
    • F02B23/0639Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom the combustion space having substantially the shape of a cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0678Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/28Other pistons with specially-shaped head
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/40Squish effect
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0621Squish flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0624Swirl flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • This invention relates to a squish jet combustion chamber for use in internal combustion engines.
  • the present invention provides a piston member or cylinder head member, which has a substantially cylindrical bowl opening onto the face of the member.
  • a pair of squish jet passages are further provided, which have respective inlets communicating with the face of the member.
  • the pair also has respective, transversely spaced, outlets directed substantially tangentially into the bowl.
  • the outlet of the first one of the pair is directed upwardly, and the outlet of a second one of the pair is directed downwardly from a position above the outlet of the first one.
  • the member as described preferably has a plurality of pairs of such squish jet passages, each pair being constructed as described.
  • the outlets of the first ones and second ones of the pairs of squish jet passages lie in respective lower and upper parallel, transverse planes.
  • the outlets of the pair of squish jets are transversely opposed. That is, they are opposed as viewed on a transverse plane from above, but not directly opposed when viewed on a vertical plane.
  • the outlets of the first and second ones of the squish jet passages of each pair are preferably adjacent to and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages.
  • the bowl is preferably disposed centrally in the face of the member.
  • the squish jet passages may also be of equal length, with the inlets of the squish jet passages being equally spaced apart on a circle concentric with the opening of the bowl.
  • a particularly preferred number of pairs of squish jet passages is four pairs.
  • the piston member or cylinder head member may be provided with a bowl opening onto the face of it.
  • a plurality of squish jet passages are provided with respective inlets communicating with the face of the member, and respective transversely spaced outlets spaced above a lower surface of the bowl and directed into the bowl.
  • the arrangement is also such that flows of gases ejected from the outlets are substantially coplanar and intercept one another above the lower surface of the bowl.
  • the outlets of the squish jet passages are symmetrically spaced apart and arranged, so that the flows of gasses ejected therefrom are on the same radial plane.
  • the bowl is usefully cylindrical and disposed centrally on the face of the member, with the squish jet passages being of equal length and the inlets thereof being equaly spaced apart on a circle concentric with the opening of the bowl.
  • a dimple having downsloping, and preferably downcurving, sides, may usefully extend upwardly from the lower surface of the bowl. This dimple has a maximum height such that an upper end of the dimple is adjacent a lower end of the flows of gasses at the point of interception thereof, so that the dimple directs gasses at the point of interception downwardly.
  • the outlets of the squish jet passages are angularly symmetrically spaced apart about the dimple so that flows of gasses ejected therefrom are on the same radial plane.
  • FIG. 1 is a plan view of a squish jet arrangement of the present invention
  • FIG. 2 is a vertical cross section along the line 2--2 of FIG. 1;
  • FIG. 3 is a vertical cross section along the line 3--3 of FIG. 1;
  • FIG. 4 is a plan view of another squish jet arrangement of the present invention.
  • FIG. 5 is a vertical cross section of a portion of an internal combustion engine wherein the piston utilizes the squish jet arrangement of FIG. 4, which arrangement is viewed along the line 5--5 of FIG. 4.
  • a member 2 which could either be a piston, or a portion of a cylinder head, is shown.
  • a substantially cylindrical bowl 6 is positioned in the center of member 2 and opens onto the face 4 thereof.
  • a plurality of pairs of squish jet passages are provided in member 2, each pair consisting of a squish jet passage 8 and a squish jet passage 14. All of the squish jet passages 8, 14 are of equal length, and have respective inlets 10 and 16, communicating with the face 4 of member 2, and equally spaced apart on a circle concentric with the opening of bowl 6.
  • the passages of each pair 8, 14 have respective, transversely opposed outlets 12, 18 directed substantially tangentially into the bowl.
  • transversely opposed is meant that when the outlets are viewed from a plane from above as in FIG. 1, they appear to be opposing one another, however this is not the case when viewed on a vertical plane as in FIGS. 2 and 3.
  • the outlet 12 of the first one 8 of each pair 8, 14 is directed upwardly, while the outlet 18 of a second one 14 of each pair 8, 14, is directed downwardly.
  • the outlets 12 of the first ones of pairs 8, 14, and outlets 18 of second ones 18 of pairs 8, 14 are adjacent to, and directed substantially orthogonally to, outlets 18 of the second ones 14 and outlets 12 of the first ones 8, respectively, of the pairs of squish jet passages 8, 14.
  • the outlets 12 of first ones 8, and the outlets 18 of the second ones 14, of the pairs 8, 14 lie in respective lower and upper parallel, transverse planes.
  • FIG. 1 through 3 The result of the arrangement shown in FIG. 1 through 3 can understood if it is assumed that member 2 for the moment is a piston in a typical 4-stroke gasoline internal combustion engine. Then, as piston 2 moves toward TDC, the air/fuel mixture which is compressed in a squish volume between the piston face 4 and cylinder head, is forced through squish jet passages 8, 14, and out through respective outlets 12, 18.
  • the result of the foregoing is the creation of a plurality of counter-rotating, bi-level swirls, as for example the ones shown with the arrows in FIG. 1.
  • FIG. 1 through 3 would work equally well if member 2 is a cylinder head. Provision of course would have to be made for valves, spark plugs, and other well known components of a typical internal combustion engine (which of course, could include a diesel engine, and a 2 or 4 cycle engine).
  • member 20 which in FIG. 5 is piston 40, is provided with a cylindrical bowl 24 disposed centrally on the face 22 of member 20 (or face 42 of piston 40 in FIG. 5).
  • Four squish jet passages 28, all of equal length, have respective inlets 30 communicating with the face 22 of member 20, or 42 of piston 40.
  • Inlets 30 are spaced apart on a circle concentric with the opening of bowl 24.
  • Squish jet passages 28 further have coplanar outlets 32 directed into the bowl and symmetrically spaced thereabout, that is, they are spaced equal distances apart as well as equal angles apart (the latter condition being referred to as "angularly symmetric").
  • the outlets are also spaced above a lower surface 26 of the bowl 24.
  • the foregoing arrangement is such that flows of gasses can be ejected from outlets 32 in directions coplanar therewith, as for example shown in FIG. 5, to intercept one another, and thereby promote mixing and turbulence.
  • the flows of gasses will of course be in the same radial plane, that is in a plane substantially perpendicular to the direction of travel of the piston.
  • a dimple 34 is provided which has downcurving sides, and which extends upwardly from the center of the lower surface 26 of the bowl 24.
  • Dimple 34 is of a height substantially equal to the distance between the lower surface 26 of bowl 24 and lowermost ends 33 of outlets 32.
  • dimple 34 downwardly directs gasses from outlets 33 which are intercepting adjacent the central axes of bowl 24 and dimple 34.
  • dimple 34 aides in the break up of such flows of gasses.
  • the foregoing flow of gasses occur of course as the piston in an internal combustion engine having such a squish jet arrangement in the piston or cylinder thereof, approaches TDC. The highly turbulent mixture is then ignited by a spark plug near TDC, and the piston begins to move back down the cylinder.
  • squish jet arrangements above have been described particularly in relation to a gasoline internal combustion engine, they may also be usefully applied to diesel engines.
  • Other possible modifications include the possibility of having a bowl of non-circular transverse cross-section, and which may not be disposed centrally on the face of the member.
  • the squish jet passage inlets may not necessarily be concentric with the opening of the bowl.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

A squish jet arrangement for an internal combustion engine is positioned on a piston member or cylinder head member thereof. A substantially cylindrical bowl opens onto the face of the member. At least one pair, and preferably a plurality of pairs, of squish jet passages are arranged to direct flows of gasses tangentially into the bowl. As first ones of the pairs of squish jet passages lie in a lower transverse plane than second ones of the pairs, a counter-rotating, bi-level swirl can be produced by the squish jet outlets. A squish jet arrangement is also provided with outlets of squish jet passages spaced above a lower surface of a bowl, and directed to eject coplanar flows of gasses therefrom, which intercept one another.

Description

FIELD OF THE INVENTION
This invention relates to a squish jet combustion chamber for use in internal combustion engines.
DESCRIPTION OF PRIOR ART
It is well known in the art of internal combustion engines to attempt to increase the rate of mixing of an air fuel mixture in the combustion chamber, immediately prior to and during the initial stages of combustion. Such an increased rate of mixing and turbulence tends to increase the rate of combustion of the mixture, resulting in increased engine efficiency as well as lower levels of exhaust pollutents. One known means for increasing the rate of such mixing and turbulence is a squish jet or equivalent arrangement. Such arrangements are disclosed for example in U.S. Pat. No. 4,195,597 to Hofbauer et al, U.S. Pat. No. 4,191,136 to Matsumoto, U.S. Pat. No. 3,132,633 to Zimmerman, U.S. Pat. No. 1,759,161 to Lang (this arrangement basically appearing to be a reverse-squish arrangement), and U.S. Pat. No. 2,505,999 to Smith. Such arrangements have in the past also included particular means to cause swirling of the gas and fuel mixture within the combustion chamber. Examples of such arrangements are shown in the Hofbauer et al previously mentioned, as well as in U.S. Pat. Nos. 4,166,436 to Yamakawa and 3,152,523 to Whitfield et al (in particular, FIG. 6 thereof). There is apparently no previous arrangment though, whereby a counter-rotating, bi-level swirl of gas/fuel mixture is produced. In addition, there has apparently been no prior disclosure of squish jet arrangements wherein the flows of gasses from the squish jets intercept one another above a lower surface of a bowl, and are coplanar which include provision for enhancing mixing of the air/fuel mixture afjacent the lower surface of a squish jet bowl.
SUMMARY OF THE INVENTION
The present invention provides a piston member or cylinder head member, which has a substantially cylindrical bowl opening onto the face of the member. A pair of squish jet passages are further provided, which have respective inlets communicating with the face of the member. The pair also has respective, transversely spaced, outlets directed substantially tangentially into the bowl. The outlet of the first one of the pair is directed upwardly, and the outlet of a second one of the pair is directed downwardly from a position above the outlet of the first one. By such an arrangement, a counter-rotating, bi-level swirl of air/fuel mxture can be produced in the bowl by the squish jet outlets.
The member as described preferably has a plurality of pairs of such squish jet passages, each pair being constructed as described. In such case, the outlets of the first ones and second ones of the pairs of squish jet passages, lie in respective lower and upper parallel, transverse planes. Preferably, the outlets of the pair of squish jets are transversely opposed. That is, they are opposed as viewed on a transverse plane from above, but not directly opposed when viewed on a vertical plane.
The outlets of the first and second ones of the squish jet passages of each pair, are preferably adjacent to and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages. Further, the bowl is preferably disposed centrally in the face of the member. In the latter case the squish jet passages may also be of equal length, with the inlets of the squish jet passages being equally spaced apart on a circle concentric with the opening of the bowl. A particularly preferred number of pairs of squish jet passages, is four pairs.
Again, the piston member or cylinder head member, may be provided with a bowl opening onto the face of it. In this case, a plurality of squish jet passages are provided with respective inlets communicating with the face of the member, and respective transversely spaced outlets spaced above a lower surface of the bowl and directed into the bowl. The arrangement is also such that flows of gases ejected from the outlets are substantially coplanar and intercept one another above the lower surface of the bowl. Preferably, the outlets of the squish jet passages are symmetrically spaced apart and arranged, so that the flows of gasses ejected therefrom are on the same radial plane.
The bowl is usefully cylindrical and disposed centrally on the face of the member, with the squish jet passages being of equal length and the inlets thereof being equaly spaced apart on a circle concentric with the opening of the bowl. A dimple having downsloping, and preferably downcurving, sides, may usefully extend upwardly from the lower surface of the bowl. This dimple has a maximum height such that an upper end of the dimple is adjacent a lower end of the flows of gasses at the point of interception thereof, so that the dimple directs gasses at the point of interception downwardly. Preferably, the outlets of the squish jet passages are angularly symmetrically spaced apart about the dimple so that flows of gasses ejected therefrom are on the same radial plane.
DRAWINGS
Embodiments of the invention will now be described with reference to the drawings, in which:
FIG. 1 is a plan view of a squish jet arrangement of the present invention;
FIG. 2 is a vertical cross section along the line 2--2 of FIG. 1;
FIG. 3 is a vertical cross section along the line 3--3 of FIG. 1;
FIG. 4 is a plan view of another squish jet arrangement of the present invention;
FIG. 5 is a vertical cross section of a portion of an internal combustion engine wherein the piston utilizes the squish jet arrangement of FIG. 4, which arrangement is viewed along the line 5--5 of FIG. 4.
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
Referring to FIGS. 1 through 3, a member 2, which could either be a piston, or a portion of a cylinder head, is shown. A substantially cylindrical bowl 6 is positioned in the center of member 2 and opens onto the face 4 thereof. A plurality of pairs of squish jet passages are provided in member 2, each pair consisting of a squish jet passage 8 and a squish jet passage 14. All of the squish jet passages 8, 14 are of equal length, and have respective inlets 10 and 16, communicating with the face 4 of member 2, and equally spaced apart on a circle concentric with the opening of bowl 6. The passages of each pair 8, 14 have respective, transversely opposed outlets 12, 18 directed substantially tangentially into the bowl. By "transversely opposed" is meant that when the outlets are viewed from a plane from above as in FIG. 1, they appear to be opposing one another, however this is not the case when viewed on a vertical plane as in FIGS. 2 and 3. The outlet 12 of the first one 8 of each pair 8, 14 is directed upwardly, while the outlet 18 of a second one 14 of each pair 8, 14, is directed downwardly. In addition, as is most apparent from FIG. 1, the outlets 12 of the first ones of pairs 8, 14, and outlets 18 of second ones 18 of pairs 8, 14, are adjacent to, and directed substantially orthogonally to, outlets 18 of the second ones 14 and outlets 12 of the first ones 8, respectively, of the pairs of squish jet passages 8, 14. Further, as is most apparent from FIGS. 2 and 3, the outlets 12 of first ones 8, and the outlets 18 of the second ones 14, of the pairs 8, 14, lie in respective lower and upper parallel, transverse planes.
The result of the arrangement shown in FIG. 1 through 3 can understood if it is assumed that member 2 for the moment is a piston in a typical 4-stroke gasoline internal combustion engine. Then, as piston 2 moves toward TDC, the air/fuel mixture which is compressed in a squish volume between the piston face 4 and cylinder head, is forced through squish jet passages 8, 14, and out through respective outlets 12, 18. The result of the foregoing is the creation of a plurality of counter-rotating, bi-level swirls, as for example the ones shown with the arrows in FIG. 1. The result is swirling helical flows of gas which are opposite one another in direction, therby generating strong shear flow resulting in creation of high intensity small-scale turbulence in bowl 6, and hence fairly rapid and effective mixing of the air/fuel mixture. Of course, the arrangement shown FIG. 1 through 3 would work equally well if member 2 is a cylinder head. Provision of course would have to be made for valves, spark plugs, and other well known components of a typical internal combustion engine (which of course, could include a diesel engine, and a 2 or 4 cycle engine).
Referring now to FIGS. 4 and 5, member 20, which in FIG. 5 is piston 40, is provided with a cylindrical bowl 24 disposed centrally on the face 22 of member 20 (or face 42 of piston 40 in FIG. 5). Four squish jet passages 28, all of equal length, have respective inlets 30 communicating with the face 22 of member 20, or 42 of piston 40. Inlets 30 are spaced apart on a circle concentric with the opening of bowl 24. Squish jet passages 28 further have coplanar outlets 32 directed into the bowl and symmetrically spaced thereabout, that is, they are spaced equal distances apart as well as equal angles apart (the latter condition being referred to as "angularly symmetric"). The outlets are also spaced above a lower surface 26 of the bowl 24. The foregoing arrangement is such that flows of gasses can be ejected from outlets 32 in directions coplanar therewith, as for example shown in FIG. 5, to intercept one another, and thereby promote mixing and turbulence. The flows of gasses will of course be in the same radial plane, that is in a plane substantially perpendicular to the direction of travel of the piston.
A dimple 34 is provided which has downcurving sides, and which extends upwardly from the center of the lower surface 26 of the bowl 24. Dimple 34 is of a height substantially equal to the distance between the lower surface 26 of bowl 24 and lowermost ends 33 of outlets 32. By virtue of the foregoing arrangement, dimple 34 downwardly directs gasses from outlets 33 which are intercepting adjacent the central axes of bowl 24 and dimple 34. Thus, dimple 34 aides in the break up of such flows of gasses. The foregoing flow of gasses occur of course as the piston in an internal combustion engine having such a squish jet arrangement in the piston or cylinder thereof, approaches TDC. The highly turbulent mixture is then ignited by a spark plug near TDC, and the piston begins to move back down the cylinder. As the piston moves down, a reverse-squish process takes place drawing enflamed mixture up through squish jet passages 28, and into a squish region between the face 22 of member 20, and the face of the other member, that is in FIG. 5, between face 42 of piston 40, and face 46 of a cylinder head 44. Such reverse squish movement aides in ignition of unburned mixture in the squish volume, and provides more complete combustion than would otherwise be possible.
An advantage of the arrangements described compared to combustion chambers utilizing swirl in the entire combustion chamber to promote turbulence, is that the squish jet turbulence in the former arrangements is generated near TDC, when such turbulence is most effective in promoting lean combustion. In contrast, swirl generated turbulence produced in the entire combustion chamber, generally decays substantially before TDC. Another advantage of the arrangements described, is that turbulence is confined largely to the center of the combustion chamber, rather than at the walls, thereby minimizing the effects of increased heat transfer to the walls.
It will be appreciated that although the squish jet arrangements above have been described particularly in relation to a gasoline internal combustion engine, they may also be usefully applied to diesel engines. Other possible modifications include the possibility of having a bowl of non-circular transverse cross-section, and which may not be disposed centrally on the face of the member. In addition, the squish jet passage inlets may not necessarily be concentric with the opening of the bowl.
As will be apparent to those skilled in the art in light of the foregoing disclosure, many further alterations and modifications are possible in the practice of this invention without departing from the spirit of scope thereof. Accordingly, the scope of the invention is to be construed in accordance with the substance defined by the following claims.

Claims (32)

I claim:
1. An internal combustion engine block having a piston and cylinder head, one of which has:
(a) a substantially cylindrical bowl opening into the face thereof;
(b) a pair of squish jet passages having respective inlets communicating with the face thereof, and respective, transversely spaced, outlets directed substantially tangentially into the bowl, the outlet of a first one of the pair being directed upwardly, and the outlet of second one of the pair being directed downwardly from a position above the outlet of the first one, so that a counter-rotating, bi-level swirl can be produced in the bowl by the squish jet outlets.
2. An internal combustion engine block as described in claim 1 wherein said one of the piston and cylinder head has a plurality of pairs of squish jet passages, each pair as described, the outlets of the first ones and the second ones of the pairs being in respective lower and upper parallel transverse planes.
3. An internal combustion engine block as described in claim 2 wherein the outlets of the pair are transversely opposed.
4. An internal combustion engine block as described in claim 3 wherein the outlets of the first and second ones of the squish jet passages of each pair, are adjacent to, and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages.
5. An internal combustion engine block as described in claim 4 wherein the bowl is disposed centrally in the face of said one, and wherein said squish jet passages are of equal length with the inlets of the squish jet passages being equally spaced apart on a circle concentric with the opening of the bowl.
6. An internal combustion engine block as described in claim 5 wherein said one has four pairs of squish jet passages.
7. A piston having:
(a) A substantially cylindrical bowl opening into the face thereof:
(b) a pair of squish jet passages having respective inlets communicating with the face thereof, and respective, transversely spaced, outlets directed substantially tangentially into the bowl, the outlet of a first one of the pair being directed upwardly, and the outlet of a second one of the pair being directed downwardly from a position above the outlet of the first one, so that a counter-rotating, bi-level swirl can be produced in the bowl by the squish jet outlets.
8. A piston as described in claim 7 wherein the outlets of the pair are transversely opposed.
9. A piston as described in claim 8 wherein the outlets of the first and second ones of the squish jet passages of each pair, are adjacent to, and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages.
10. A piston having:
(a) a substantially cylindrical bowl disposed centrally in the face of the piston;
(b) a plurality of pairs of squish jet passages of equal length, and having respective inlets communicating with the face of the piston and equally spaced apart on a circle concentric with the opening of the bowl, the passages of each pair having respective, transversely opposed outlets directed substantially tangentially into the bowl, with the outlet of a first one of each pair being directed upwardly, and the outlet of a second one of each pair being directed downwardly, the outlets of the first and second ones of each pair being adjacent to, and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages, and the outlets of the first ones and second ones of the pairs being in respective lower and upper parallel transverse planes, so that a counter-rotating bi-level swirl can be produced in the bowl by the squish jet passages.
11. A cylinder head having:
(a) a substantially cylindrical bowl opening into the face thereof;
(b) a pair of squish jet passages having respective inlets communicating with the face thereof, and respective, transversely spaced, outlets directed substantially tangentially into the bowl, the outlet of a first one of the pair being directed upwardly, and the outlet of a second one of the pair being directed downwardly from a position above the outlet of the first one, so that a counter-rotating, bi-level swirl can be produced in the bowl by the squish jet outlets.
12. A cylinder head described in claim 11 wherein the outlets of the pair are transversely opposed.
13. A cylinder head as described in claim 12 wherein the outlets of the first and second ones of the squish jet passages of each pair, are adjacent to, and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages.
14. A cylinder head having:
(a) a substantially cylindrical bowl disposed centrally in the face of the cylinder head:
(b) a plurality of pairs of squish jet passages of equal length, and having respective inlets communicating with the face of the cylinder head and equally spaced apart on a circle concentric with the opening of the bowl, the passages of each pair having respective, transversely opposed outlets directed substantially tangentially into the bowl, with the outlet of a first one of each pair being directed upwardly, and the outlet of a second one of each pair being directed downwardly, the outlets of the first and second ones of each pair being adjacent to, and directed substantially orthogonally to, outlets of the second and first ones, respectively, of other pairs of the squish jet passages, and the outlets of the first ones and second ones of the pairs being in respective lower and upper parallel transverse planes, so that a counter-rotating bi-level swirl can be produced in the bowl by the squish jet passages.
15. A piston as described in claim 10 which has four pairs of squish jet passages.
16. A cylinder head as described in claim 14 which has four pairs of squish jet passages.
17. A internal combustion engine block having a piston and cylinder head, one of which has:
(a) a bowl opening onto the face thereof:
(b) a plurality of squish jet passages having respective inlets disposed at spaced apart positions on the face thereof, and respective transversely spaced outlets above a lower surface of the bowl and directed into the bowl, so that flows of gasses ejected therefrom are substantially coplanar and intercept one another above the lower surface of the bowl
the other one of the piston and cylinder head being shaped so that as the piston approaches top dead center, gasses are forced through the inlets of the squish jet passages, to be ejected from the outlets thereof.
18. An internal combustion engine block as described in claim 17 wherein the outlets of the squish jet passages are symmetrically spaced apart and arranged so that the flows of gasses ejected therefrom are on the same radial plane.
19. An internal combustion engine block as described in claim 18 wherein the bowl is cylindrical and disposed centrally in the face of said one, and the squish jet passages are of equal length with the inlets thereof being equally spaced apart on a circle concentric with the opening of the bowl.
20. A piston having:
(a) a bowl opening onto the face thereof;
(b) a plurality of squish jet passages having respective inlets disposed at spaced apart positions on the face thereof, and respective transversely spaced outlets spaced above a lower surface of the bowl and directed into the bowl, so that flows of gasses ejected therefrom are substantially coplanar and intercept one another above the lower surface of the bowl.
21. An internal combustion engine block as described in 14 wherein the outlets of the squish jet passages are symmetrically spaced apart and arranged so that the flows of gasses ejected therefrom are on the same radial plane.
22. An internal combustion engine block as described in claim 21 wherein the bowl is cylindrical and disposed centrally in the face of said one, the squish jet passages are of equal length with the inlets thereof being equally spaced apart on a circle concentric with the opening of the bowl.
23. A cylinder head having:
(a) a bowl opening onto the face thereof;
(b) a plurality of squish jet passages having respective inlets disposed at spaced apart positions on the face thereof, and respective transversely spaced outlets spaced above a lower surface of the bowl and directed into the bowl, so that flows of gasses ejected therefrom are substantially coplanar and intercept one another above the lower surface of the bowl.
24. A cylinder head as described in claim 23 wherein the outlets of the squish jet passages are symmetrically spaced apart and arranged so that the flows of gasses ejected therefrom are on the same readial plane.
25. A cylinder head as described in claim 24 wherein the bowl is cylindrical and disposed centrally in the face of the cylinder head, and the squish jet passages are of equal length with the inlets thereof being equally spaced apart on a circle concentric with the opening of the bowl.
26. An internal combustion engine block as described in claim 17 additionally comprising a dimple having downsloping sides, extending upwardly from the lower surface of the bowl, and having a maximum height such that an upper end of said simple is adjacent a lower end of the flows of gasses at the point of interception, and the dimple directs gasses thereat downwardly.
27. An internal combustion engine block as described in claim 26 wherein the outlets of the squish jet passages are angularly symmetrically spaced apart about said dimple, and arranged so that the flows of gasses ejected therefrom are on the same radial plane.
28. An internal combustion engine block as described in claim 27 wherein the bowl is cylindrical and disposed centrally in the face of said one, and the squish jet passages are of equal length with the inlets thereof being equally spaced apart on a circle concentric with the opening of the bowl.
29. A piston as described in claim 20 additionally comprising a dimple having downcurving sides, extending upwardly from the lower surface of the bowl, and having a maximum height such that an upper end of said dimple is adjacent a lower end of the flows of gasses at the point of interception, and the dimple directs gasses thereat downwardly.
30. A piston as described in claim 29 wherein the outlets of the squish jet passages are angularly symmetrically spaced apart about said dimple, and arranged so that the flows of gasses ejected therefrom are on the same radial plane.
31. A cylinder head as described in claim 23 additionally comprising a dimple having downcurving sides, extending upwardly from the lower surface of the bowl, and having a maximum height such that an upper end of said dimple is adjacent a lower end of the flows of gasses at the point of interception, and the dimple directs gasses thereat downwardly.
32. A cylinder head as described in claim 31 wherein the outlets of the squish jet passages are angularly symmetrically spaced apart about said dimple, and arranged so that the flows of gasses ejected therefrom are on the same radial plane.
US06/623,740 1984-06-22 1984-06-22 Internal combustion engine squish jet combustion chamber Expired - Fee Related US4572123A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US06/623,740 US4572123A (en) 1984-06-22 1984-06-22 Internal combustion engine squish jet combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/623,740 US4572123A (en) 1984-06-22 1984-06-22 Internal combustion engine squish jet combustion chamber

Publications (1)

Publication Number Publication Date
US4572123A true US4572123A (en) 1986-02-25

Family

ID=24499235

Family Applications (1)

Application Number Title Priority Date Filing Date
US06/623,740 Expired - Fee Related US4572123A (en) 1984-06-22 1984-06-22 Internal combustion engine squish jet combustion chamber

Country Status (1)

Country Link
US (1) US4572123A (en)

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4669431A (en) * 1986-01-23 1987-06-02 Stephen Simay Internal combustion engine with dual combustion chambers
EP0286745A1 (en) * 1987-04-14 1988-10-19 Stephen E. Simay Internal combustion engine
US4898135A (en) * 1989-02-16 1990-02-06 Sonex Research, Inc. Piston and process for achieving controlled ignition and combustion of hydrocarbon fuels in internal combustion engines by generation and management of fuel radical species
FR2639681A1 (en) * 1988-11-29 1990-06-01 Renault Vehicules Ind Piston for a diesel engine
US5065715A (en) * 1990-02-07 1991-11-19 The University Of British Columbia Squish jet combustion chamber
US5103784A (en) * 1990-02-07 1992-04-14 The Univeristy Of British Columbia Squish jet combustion chamber
EP0598605A1 (en) * 1992-11-19 1994-05-25 Isuzu Ceramics Research Institute Co., Ltd. Pre-chamber type engine
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
US5692468A (en) * 1995-07-25 1997-12-02 Outboard Marine Corporation Fuel-injected internal combustion engine with improved combustion
US6435159B1 (en) 2000-05-10 2002-08-20 Bombardier Motor Corporation Of America Fuel injected internal combustion engine with reduced squish factor
US6832589B2 (en) 2001-06-06 2004-12-21 Textron Lycoming, A Division Of Avco Corporation Cylinder assembly for an aircraft engine
US20050081819A1 (en) * 2003-10-16 2005-04-21 Kim Tae-Gyun Piston structure of engine
US20060169257A1 (en) * 2005-01-28 2006-08-03 Ziehl John C High compression pistons having vanes or channels
US7284524B2 (en) 2005-02-25 2007-10-23 Lycoming Engines, A Division Of Avco Corporation Cylinder head assemblies
US7581526B2 (en) 2005-09-01 2009-09-01 Harry V. Lehmann Device and method to increase fuel burn efficiency in internal combustion engines
US20110265770A1 (en) * 2008-12-31 2011-11-03 Joey Malfa Internal combustion engine
US8528514B1 (en) 2012-08-07 2013-09-10 New Age Technology LLC Piston for reciprocating engines
US20170107938A1 (en) * 2015-10-15 2017-04-20 The Regents Of The University Of Michigan Lean burn internal combustion engine
US9909489B1 (en) 2016-10-05 2018-03-06 Caterpillar Inc. Piston fluid passages for reduced soot
FR3057913A1 (en) * 2016-10-20 2018-04-27 Renault S.A.S PISTON FOR INTERNAL COMBUSTION ENGINE WITH AERODYNAMIC CURTAIN
US10316734B2 (en) 2016-10-05 2019-06-11 Caterpillar Inc. Piston and cylinder features for enhanced squish flow
US10393063B2 (en) * 2017-09-25 2019-08-27 Somender Singh Internal combustion engine piston with chamber
US20200025064A1 (en) * 2018-07-18 2020-01-23 Warren Engine Company Fuel ignition methods for opposed piston engines and related structures
US11572848B1 (en) * 2021-11-04 2023-02-07 Edric Darrell Culbreth Multi-port power engine

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB475179A (en) * 1935-02-09 1937-11-12 Alfred Buechi Improvements in or relating to the combustion chambers of four stroke cycle internal combustion engines
US2133478A (en) * 1935-10-31 1938-10-18 Adlerwerke Kleyer Ag H Internal combustion engine
US2505999A (en) * 1944-09-22 1950-05-02 Frank J Smith Diesel engine for aircraft
US2738782A (en) * 1952-02-25 1956-03-20 Jr Albert G Bodine Detonation suppression means for internal combustion engines
FR1287172A (en) * 1961-04-24 1962-03-09 Maschf Augsburg Nuernberg Ag Combustion engine with air compression and injection of liquid fuel into a pre-combustion chamber separate from the working chamber of the engine
US3195520A (en) * 1963-04-03 1965-07-20 Ford Motor Co Internal combustion engine combustion chambers
US4009702A (en) * 1974-11-15 1977-03-01 Texaco Inc. Piston with turbulence inducing face configuration
JPS5442505A (en) * 1977-09-09 1979-04-04 Toyota Motor Corp Combustion chamber of internal combustion engine
US4166436A (en) * 1976-11-15 1979-09-04 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
JPS5756616A (en) * 1980-09-17 1982-04-05 Daihatsu Motor Co Ltd Swirl-chamber diesel engine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB475179A (en) * 1935-02-09 1937-11-12 Alfred Buechi Improvements in or relating to the combustion chambers of four stroke cycle internal combustion engines
US2133478A (en) * 1935-10-31 1938-10-18 Adlerwerke Kleyer Ag H Internal combustion engine
US2505999A (en) * 1944-09-22 1950-05-02 Frank J Smith Diesel engine for aircraft
US2738782A (en) * 1952-02-25 1956-03-20 Jr Albert G Bodine Detonation suppression means for internal combustion engines
FR1287172A (en) * 1961-04-24 1962-03-09 Maschf Augsburg Nuernberg Ag Combustion engine with air compression and injection of liquid fuel into a pre-combustion chamber separate from the working chamber of the engine
US3195520A (en) * 1963-04-03 1965-07-20 Ford Motor Co Internal combustion engine combustion chambers
US4009702A (en) * 1974-11-15 1977-03-01 Texaco Inc. Piston with turbulence inducing face configuration
US4166436A (en) * 1976-11-15 1979-09-04 Toyota Jidosha Kogyo Kabushiki Kaisha Combustion chamber of an internal combustion engine
JPS5442505A (en) * 1977-09-09 1979-04-04 Toyota Motor Corp Combustion chamber of internal combustion engine
JPS5756616A (en) * 1980-09-17 1982-04-05 Daihatsu Motor Co Ltd Swirl-chamber diesel engine

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4669431A (en) * 1986-01-23 1987-06-02 Stephen Simay Internal combustion engine with dual combustion chambers
EP0286745A1 (en) * 1987-04-14 1988-10-19 Stephen E. Simay Internal combustion engine
FR2639681A1 (en) * 1988-11-29 1990-06-01 Renault Vehicules Ind Piston for a diesel engine
US4898135A (en) * 1989-02-16 1990-02-06 Sonex Research, Inc. Piston and process for achieving controlled ignition and combustion of hydrocarbon fuels in internal combustion engines by generation and management of fuel radical species
US5065715A (en) * 1990-02-07 1991-11-19 The University Of British Columbia Squish jet combustion chamber
US5103784A (en) * 1990-02-07 1992-04-14 The Univeristy Of British Columbia Squish jet combustion chamber
US5322042A (en) * 1992-06-17 1994-06-21 Sonex Research, Inc. Combustion chamber for internal combustion engine and process of combustion using fuel radical species
EP0598605A1 (en) * 1992-11-19 1994-05-25 Isuzu Ceramics Research Institute Co., Ltd. Pre-chamber type engine
US5425337A (en) * 1992-11-19 1995-06-20 Izusu Ceramics Research Institute Co., Ltd. Pre-chamber type engine
US5692468A (en) * 1995-07-25 1997-12-02 Outboard Marine Corporation Fuel-injected internal combustion engine with improved combustion
US6435159B1 (en) 2000-05-10 2002-08-20 Bombardier Motor Corporation Of America Fuel injected internal combustion engine with reduced squish factor
US6832589B2 (en) 2001-06-06 2004-12-21 Textron Lycoming, A Division Of Avco Corporation Cylinder assembly for an aircraft engine
US20050081819A1 (en) * 2003-10-16 2005-04-21 Kim Tae-Gyun Piston structure of engine
US7004140B2 (en) * 2003-10-16 2006-02-28 Hyundai Motor Company Piston structure of engine
US20060169257A1 (en) * 2005-01-28 2006-08-03 Ziehl John C High compression pistons having vanes or channels
US7284524B2 (en) 2005-02-25 2007-10-23 Lycoming Engines, A Division Of Avco Corporation Cylinder head assemblies
US7581526B2 (en) 2005-09-01 2009-09-01 Harry V. Lehmann Device and method to increase fuel burn efficiency in internal combustion engines
US20110265770A1 (en) * 2008-12-31 2011-11-03 Joey Malfa Internal combustion engine
US8813718B2 (en) * 2008-12-31 2014-08-26 Speed Of Air, Inc. Internal combustion engine
US9303594B2 (en) 2008-12-31 2016-04-05 Speed Of Air, Inc. Internal combustion engine
US8528514B1 (en) 2012-08-07 2013-09-10 New Age Technology LLC Piston for reciprocating engines
US20170107938A1 (en) * 2015-10-15 2017-04-20 The Regents Of The University Of Michigan Lean burn internal combustion engine
US10066580B2 (en) * 2015-10-15 2018-09-04 The Regents Of The University Of Michigan Lean burn internal combustion engine
US9909489B1 (en) 2016-10-05 2018-03-06 Caterpillar Inc. Piston fluid passages for reduced soot
US10316734B2 (en) 2016-10-05 2019-06-11 Caterpillar Inc. Piston and cylinder features for enhanced squish flow
FR3057913A1 (en) * 2016-10-20 2018-04-27 Renault S.A.S PISTON FOR INTERNAL COMBUSTION ENGINE WITH AERODYNAMIC CURTAIN
US10393063B2 (en) * 2017-09-25 2019-08-27 Somender Singh Internal combustion engine piston with chamber
US20200025064A1 (en) * 2018-07-18 2020-01-23 Warren Engine Company Fuel ignition methods for opposed piston engines and related structures
US10989109B2 (en) * 2018-07-18 2021-04-27 Warren Engine Company Fuel ignition methods for opposed piston engines and related structures
US11572848B1 (en) * 2021-11-04 2023-02-07 Edric Darrell Culbreth Multi-port power engine

Similar Documents

Publication Publication Date Title
US4572123A (en) Internal combustion engine squish jet combustion chamber
US4324214A (en) Combustion chamber for an internal combustion engine
US4359027A (en) Two-cycle internal combustion engine having high swirl combustion chamber
US4625693A (en) Internal combustion engine
US4170968A (en) Internal combustion engine with an auxiliary combustion chamber
US4237827A (en) Swirl-chamber diesel engine with piston formed with curved groove at its crown
US6199544B1 (en) Combustion chamber system having an improved configuration with squish areas
US4452221A (en) High squish dual swirl engine combustion chamber
US4635591A (en) Internal-combustion engines
US4005684A (en) Internal combustion engine
SU1075992A3 (en) Internal combustion engine
US4686941A (en) Turbulence generator for two-stroke spark-assisted diesel engines
US4175531A (en) Internal combustion engine with an auxiliary combustion chamber
US4267806A (en) High compression type internal combustion engine
US4913111A (en) Turbulence generator for two-stroker spark-assisted diesel engines
US4116181A (en) Dual spark plug ignition internal combustion engine
US5613471A (en) Diesel engine using fuel jet impingement and diffusion
EP0075643A2 (en) Internal combustion engine
GB1561729A (en) Pre-combustion chamber diesel engines
US4125105A (en) Four cycle internal combustion engine
JPH02140429A (en) Twin piston two-cycle engine
US4433647A (en) Internal combustion motor with turbulence chamber
JPH0518245A (en) Injection-in-cylinder type internal combustion engine
JPH0115862Y2 (en)
US4355604A (en) Shrouded valve for internal combustion engine

Legal Events

Date Code Title Description
AS Assignment

Owner name: UNIVERSITY OF BRITISH COLUMBIA THE, 2075 WESBROOK

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:EVANS, ROBERT L.;REEL/FRAME:004278/0080

Effective date: 19840521

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY

FPAY Fee payment

Year of fee payment: 4

REMI Maintenance fee reminder mailed
REMI Maintenance fee reminder mailed
LAPS Lapse for failure to pay maintenance fees
FP Lapsed due to failure to pay maintenance fee

Effective date: 19940227

STCH Information on status: patent discontinuation

Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362